GB191000135A - Improvements relating to Turbines. - Google Patents

Improvements relating to Turbines.

Info

Publication number
GB191000135A
GB191000135A GB191000135DA GB191000135A GB 191000135 A GB191000135 A GB 191000135A GB 191000135D A GB191000135D A GB 191000135DA GB 191000135 A GB191000135 A GB 191000135A
Authority
GB
United Kingdom
Prior art keywords
rotor
nozzles
passages
steam
blades
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
Inventor
Paul Brat
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Application granted granted Critical
Publication of GB191000135A publication Critical patent/GB191000135A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

135. Brat, P. Jan. 3. Circular-flow type; combined-flow type.-In a turbine in which the motive fluid is supplied to reaction nozzles in the rotor, the fluid issuing from the nozzles is redirected upon blades on the rotor by stationary guide-blades. In the construction shown in Fig. 2, the steam issuing from the nozzles f in the rotor b is redirected by baffles g upon blades k behind the nozzles. As shown in Fig. 6, steam is admitted at d<1> to the nozzles f, and the stationary passages n deflect it into passages k in the rotor, and so on, thus producing a turbine of the circular-flow type. The nozzles f may be in the centre of the rotor, two sets of passages n, k being provided. A channel e<2>, Fig. 5, having a number of pockets e<1> is cut in the rotor between the entrances e of the nozzles f. In a further modification, the passages n deflect the steam upon radial blades on the periphery of the rotor, the steam being then further expanded in an axial-flow turbine of the ordinary type.
GB191000135D 1910-01-03 1910-01-03 Improvements relating to Turbines. Expired GB191000135A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB191000135T 1910-01-03

Publications (1)

Publication Number Publication Date
GB191000135A true GB191000135A (en) 1910-08-11

Family

ID=32448088

Family Applications (1)

Application Number Title Priority Date Filing Date
GB191000135D Expired GB191000135A (en) 1910-01-03 1910-01-03 Improvements relating to Turbines.

Country Status (1)

Country Link
GB (1) GB191000135A (en)

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